ENGINEERING RESEARCH-DEVELOP FUEL TANK AND PRESSURE CABIN SEALING METHODS FOR HIGH TEMPERATURE USE
Abstract
An inv tigation as made to develop fuel tank and pressure cabin sealing methods for high temperature use. Various sealing materials and methods for use in the temperature range of -100 to 1000 F were examined including (1) a fastener test met o an (2) a silicone sealant. a from a k s li g evaluation re pres nted (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 10, 1962
- Accession Number
- AD0277486
Entities
People
- M.t. Carroll
Organizations
- General Dynamics